Effect of Autoclave Processing Parameters used to Form Hybrid SIAL Parts on the Structure and Properties of Al-Li Alloy 1441 Sheets

The paper considers the main stages of developing hybrid composite materials similar to GLARE, such as SIAL, on the basis of alloy 1441 sheets. The technology of manufacturing aviation products via auto-clave forming of such materials includes additional episodes of heating the thermally processed alloy 1441 sheets that form part of the hybrid material structure. Studying the microstructure of the Al-Li alloy sheets, the number of emergent phases and their mechanical properties shows that there is no considerable variation to be found in the properties of the SIAL hybrid composite material as a result of the alteration taking place The work is performed as part of actualising a comprehensive field of research 6.2 "Laminate fracture-resistant, high-strength metal-polymer materials" ("Strategic areas of developing materials and material processing technology for the period up to 2030")

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Tensile Properties of Woven Carbon/Kevlar Reinforced Epoxy Hybrid Composite

Materials Science Forum ◽

10.4028/www.scientific.net/msf.890.20 ◽

2017 ◽

Vol 890 ◽

pp. 20-23 ◽

Cited By ~ 3

Author(s):

Nurain Hashim ◽

Dayang Laila Abdul Majid ◽

Rizal Zahari ◽

Noorfaizal Yidris

Keyword(s):

Composite Material ◽

Hybrid Composite ◽

Impact Resistance ◽

High Strength ◽

Tensile Behaviour ◽

Carbon Fibres ◽

Fibre Direction ◽

Hybrid Effect ◽

Hybrid Composite Material ◽

Selection Of

Carbon fibres and Kevlar fibres are among the commonly used fibres in the composite industry. As carbon fibres usually known for its superior strength, its low impact resistance limited its application in the industry. However, further research found that combining the high strength fibres with more ductile fibres like Kevlar could improve the material’s impact resistance. This hybrid effect was also found to be most effective by using intra-ply woven hybrid fibres in the composite. In this work, hybrid composite material was fabricated by using woven carbon-Kevlar cloths with epoxy matrix and the mechanical properties are determined at 0 ̊, 45 ̊ and 90 ̊. The hybrid composite material was found to have highest tensile strength at 0 ̊ (carbon) direction. As the material’s strength and tensile behaviour are different at every fibre types, the selection of fibre direction of the woven cloth in loading is an important criteria in any applications.

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Optimization of Hybrid Composite Material Structure for Wing Skin of Tourist Class Reusable Space Vehicle

Herald of the Bauman Moscow State Technical University Series Mechanical Engineering ◽

10.18698/0236-3941-2018-1-4-19 ◽

2018 ◽

pp. 4-19 ◽

Cited By ~ 3

Author(s):

Т Г Агеева ◽

◽

Е Р Ашихмина ◽

П В Просунцов ◽

◽

...

Keyword(s):

Composite Material ◽

Hybrid Composite ◽

Space Vehicle ◽

Material Structure ◽

Hybrid Composite Material ◽

Wing Skin

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PREDICTION, BY A GENETIC ALGORITHM, OF THE EFFECT OF HEAT STRESS ON THE TRANSVERSE DAMAGE OF FIBER-MATRIX INTERFACE OF HYBRID COMPOSITE MATERIAL (GLASS-CARBON/ EPOXY)

Composites Mechanics Computations Applications An International Journal ◽

10.1615/compmechcomputapplintj.v7.i1.30 ◽

2016 ◽

Vol 7 (1) ◽

pp. 31-43

Author(s):

M. Morsli ◽

A. Mokaddem ◽

B. Doumi ◽

L. Temimi ◽

A. Boutaous ◽

...

Keyword(s):

Genetic Algorithm ◽

Composite Material ◽

Heat Stress ◽

Hybrid Composite ◽

Matrix Interface ◽

Hybrid Composite Material ◽

Glass Carbon ◽

Fiber Matrix Interface ◽

Fiber Matrix ◽

Transverse Damage

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Promising hybrid fabrics based on carbon and aramid fibers as a reinforcing filler for polymer composites

Voprosy Materialovedeniya ◽

10.22349/1994-6716-2019-98-2-86-95 ◽

2019 ◽

pp. 86-95 ◽

Cited By ~ 1

Author(s):

G. F. Zhelezina ◽

V. G. Bova ◽

S. I. Voinov ◽

A. Ch. Kan

Keyword(s):

Composite Material ◽

Polymer Composites ◽

Carbon Fibers ◽

Mechanical Characteristics ◽

High Strength ◽

High Modulus ◽

Hybrid Composite Material ◽

Hybrid Fabric ◽

Reinforcing Filler ◽

Physical And Mechanical Characteristics

The paper considers possibilities of using a hybrid fabric made of high-modulus carbon yarn brand ZhGV and high-strength aramid yarns brand Rusar-NT for polymer composites reinforcement. The results of studies of the physical and mechanical characteristics of hybrid composite material and values of the implementation of the strength and elasticity carbon fibers and aramid module for composite material are presented.

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